Passive Hub Flapping Lock

ABSTRACT

The present invention includes a passive hub flapping lock including stop wedges; frames coupled to the stop wedges; rods coupled to the frames, and each rod comprising a bracket; lever arms, each lever arm rotatably coupled to a pivot and coupled at a first lever arm end to one of the rods at the bracket of the rod; weight sets, each weight set coupled to a second lever arm end; and pivot torsion springs, each pivot torsion spring positioned at a pivot and biased to hold the flapping lock in an engaged position when stationary or at a rotational speed below a specified rotational speed; wherein the flapping lock is in an engaged position below the specified rotational speed and in a disengaged position above the specified rotational speed and the weight sets move outward, rotating the lever arms.

CROSS-REFERENCE TO RELATED APPLICATIONS

Not applicable.

STATEMENT OF FEDERALLY FUNDED RESEARCH

Not applicable.

TECHNICAL FIELD OF THE INVENTION

The present invention relates in general to the field of aircraftpropulsion. In particular, the present invention relates to mast sleevesin rotorcraft.

BACKGROUND OF THE INVENTION

Without limiting the scope of the invention, its background is describedin connection with rotorcraft with rotors that may be folded fortransport.

When rotors in rotorcraft are stationary or rotating slowly, includingwhen the rotors are folded and secured for stowage, there exists thepossibility the rotor will flap and contact the mast sleeve, with thepossibility of damage to the mast sleeve, the rotor, or both. A devicefor preventing such contact that is relatively lightweight and operatesautomatically is desirable.

SUMMARY OF THE INVENTION

In some embodiments of the disclosure, a passive hub flapping lock isdisclosed as including one or more stop wedges; one or more framescoupled to the one or more stop wedges; one or more rods coupled to theone or more frames, and each rod comprising a bracket; one or more leverarms, each lever arm rotatably coupled to a pivot and coupled at a firstlever arm end to one of the one or more rods at the bracket of the rod;one or more weight sets, each weight set coupled to a second lever armend; and one or more pivot torsion springs, each pivot torsion springpositioned at a pivot and biased to hold the flapping lock in an engagedposition when stationary or at a rotational speed below a specifiedrotational speed; wherein the flapping lock is in an engaged positionwhen stationary or at a rotational speed below the specified rotationalspeed and wherein the flapping lock is in a disengaged position when ata rotational speed above the specified rotational speed and the one ormore weight sets move outward, rotating the one or more lever arms. Inone aspect, the one or more stop wedges comprise an elastomericmaterial, a foam, a soft metal, or a combination of two or more of thosematerials. In another aspect, the one or more rods are held in place orstabilized by one or more rod sleeves. In another aspect, at least aportion of each of the one or more rod sleeves adjacent to a mast sleeveor a mast is coated with one or more substances to reduce a friction ofa motion of the one or more rod sleeves against the mast sleeve or themast. In another aspect, the rod sleeves comprise linear ball bearings.In another aspect, each of the one or more lever arms is coupled to oneof the one or more rods with a roller bearing directly or with a link.In another aspect, each of the one or more weight sets is adjustable toset the specified rotational speed. In another aspect, at least aportion of a mast sleeve, a mast, or each frame is coated with one ormore substances to reduce a friction of a motion of the one or moreframes against the mast sleeve or the mast.

In some embodiments of the disclosure, a method of preventing rotorflapping is disclosed as including providing one or more stop wedgesmounted on one or more frames to be inserted into a space between a mastsleeve or a mast and a rotor yoke to prevent hub flapping; lowering theone or more stop wedges into the space when stationary or at arotational speed below a specified rotational speed; raising the one ormore stop wedges out of the space at the specified rotational speed;keeping the one or more stop wedges out of the space when above thespecified rotational speed; and controlling a position of the one ormore stop wedges with one or more weight sets coupled to one or morelever arms that are coupled to the one or more stop wedges, wherein theone or more weight sets move outward at the specified rotational speed,moving the lever arms such that the one or more stop wedges are raisedfrom the space. In one aspect, the one or more stop wedges comprise anelastomeric material, a foam, a soft metal, or a combination of two ormore of those materials. In another aspect, one or more rods couple theone or more stop wedges with the one or more lever arms. In anotheraspect, each of the one or more lever arms is coupled to one of the oneor more rods with a roller bearing directly or with a link. In anotheraspect, the one or more rods are held in place or stabilized by one ormore rod sleeves. In another aspect, at least a portion of each of theone or more rod sleeves adjacent to the mast sleeve or the mast iscoated with one or more substances to reduce a friction of a motion ofthe one or more rod sleeves against the mast sleeve or the mast. Inanother aspect, the one or more sleeves comprise linear ball bearings.In another aspect, each of the one or more weight sets is adjustable toset the specified rotational speed. In another aspect, at least aportion of the mast sleeve, the mast, or each frame is coated with oneor more substances to reduce a friction of a motion of the one or moreframes against the mast sleeve or the mast.

In some embodiments of the disclosure, a rotorcraft is disclosed asincluding a fuselage; one or more engines coupled to the fuselage; eachof the one or more rotor assemblies comprising a flapping lock, theflapping lock comprising: one or more stop wedges; one or more framescoupled to the one or more stop wedges; one or more rods coupled to theone or more frames, and each rod comprising a bracket; one or more leverarms, each lever arm rotatably coupled to a pivot and coupled at a firstlever arm end to one of the one or more rods at the bracket of the rod;one or more weight sets, each weight set coupled to a second lever armend; and one or more pivot torsion springs, each pivot torsion springpositioned at a pivot and biased to hold the flapping lock in an engagedposition when stationary or at a rotational speed below a specifiedrotational speed; wherein the flapping lock is in an engaged positionwhen stationary or at a rotational speed below the specified rotationalspeed and in a disengaged position when at a rotational speed above thespecified rotational speed and the one or more weight sets move outward,rotating the one or more lever arms.

In addition to the foregoing, various other method, system, andapparatus aspects are set forth in the teachings of the presentdisclosure, such as the claims, text, and drawings forming a part of thepresent disclosure.

The foregoing is a summary and thus contains, by necessity,simplifications, generalizations, and omissions of detail. Consequently,those skilled in the art will appreciate that this summary isillustrative only and is not intended to be in any way limiting. Thereaspects, features, and advantages of the devices, processes, and othersubject matter described herein will be become apparent in the teachingsset forth herein.

BRIEF DESCRIPTION OF THE DRAWINGS

For a more complete understanding of the features and advantages of thepresent invention, reference is now made to the detailed description ofthe invention along with the accompanying figures, in which:

FIG. 1 shows a side view of a helicopter according to a particularembodiment of the present invention.

FIG. 2 shows a partial cross-section, perspective view of a helicopteraccording to an embodiment of the present invention.

FIG. 3A shows a perspective view of a first tiltrotor aircraft in whichthe rotor system is in a takeoff-and-landing mode or hover modeaccording to a particular embodiment of the present invention.

FIG. 3B shows a perspective view of the first tiltrotor aircraft inwhich the rotor system is in a cruise mode according to a particularembodiment of the present invention.

FIG. 4A shows a perspective view of a second tiltrotor aircraft in whichthe rotor system is in a takeoff-and-landing mode or hover modeaccording to a particular embodiment of the present invention.

FIG. 4B shows a perspective view of the second tiltrotor aircraft inwhich the rotor system is in a cruise mode according to a particularembodiment of the present invention.

FIG. 5 illustrates a perspective view of an embodiment of the presentinvention in its disengaged position.

FIG. 6 illustrates a portion of an embodiment of the present inventionshown in FIG. 5.

FIG. 7A depicts a perspective view of an embodiment of the presentinvention in its engaged position.

FIG. 7B depicts a perspective view of an embodiment of the presentinvention in its disengaged position.

FIG. 8 illustrates a flowchart of a method embodiment of the presentinvention.

DETAILED DESCRIPTION OF THE INVENTION

Illustrative embodiments of the system of the present application aredescribed below. In the interest of clarity, not all features of anactual implementation are described in this specification. It will ofcourse be appreciated that in the development of any such actualembodiment, numerous implementation-specific decisions must be made toachieve the developer's specific goals, such as compliance withsystem-related and business-related constraints, which will vary fromone implementation to another. Moreover, it will be appreciated thatsuch a development effort might be complex and time-consuming but wouldnevertheless be a routine undertaking for those of ordinary skill in theart having the benefit of this disclosure.

In the specification, reference may be made to the spatial relationshipsbetween various components and to the spatial orientation of variousaspects of components as the devices are depicted in the attacheddrawings. However, as will be recognized by those skilled in the artafter a complete reading of the present application, the devices,members, apparatuses, etc. described herein may be positioned in anydesired orientation. Thus, the use of terms such as “above,” “below,”“upper,” “lower,” or other like terms to describe a spatial relationshipbetween various components or to describe the spatial orientation ofaspects of such components should be understood to describe a relativerelationship between the components or a spatial orientation of aspectsof such components, respectively, as the device described herein may beoriented in any desired direction.

FIGS. 1, 2, 3A, 3B, 4A, and 4B illustrate non-limiting examples ofrotorcraft with which the present invention may be used.

FIG. 1 shows an aircraft 100 in accordance with a preferred embodimentof the present application. In the exemplary embodiment, aircraft 100 isa helicopter having a fuselage 102 and a rotor system 104 carriedthereon. A plurality of rotor blades 106 is operably associated with arotor system 104 for creating flight. A tail boom 108 is depicted thatfurther includes tail rotor 110.

For example, FIG. 2 shows a partial cross-section perspective view ofaircraft 100 that includes additional detail of the present invention.Aircraft 100 further includes a rotor mast 112, which is connected tothe main rotor gearbox 114 via a main rotor mast. The main rotor gearbox114 is connected to one or more accessory gear boxes 116 and one or morereduction gearboxes 216 a, 216 b. Each reduction gearbox 216 a, 216 b isconnected to one or more engines 120 a, 120 b, which are within anengine compartment 118. A tail rotor drive shaft 122 transmitsmechanical rotation to the tail rotor gear box 124, which is connectedvia tail rotor drive shaft 126 and intermediate gear box 128.

FIGS. 3A and 3B show a tiltrotor aircraft 300 that utilizes the systemand methods in accordance with the present invention. FIG. 3Aillustrates the tiltrotor aircraft 300 in takeoff-and-landing mode orhover mode, and FIG. 3B depicts the tiltrotor aircraft 300 in cruisemode. Tiltrotor aircraft 300 includes proprotor assemblies 302 a and 302b that are carried by wings 304 a and 304 b, and are disposed at endportions 306 a and 306 b of wings 304 a and 304 b, respectively.Proprotor assemblies 302 a and 302 b include nacelles 308 a and 308 b,which carry the engines and transmissions of tiltrotor aircraft 300.Proprotor assemblies 302 a and 302 b move or rotate relative to wings304 a and 304 b between a helicopter or hover mode in which proprotorassemblies 302 a and 302 b are tilted upward, such that tiltrotoraircraft 300 flies like a conventional helicopter; and an airplane orcruise mode in which proprotor assemblies 302 a and 302 b are tiltedforward, such that tiltrotor aircraft 300 flies like a conventionalpropeller driven aircraft.

FIGS. 4A and 4B show another tiltrotor aircraft 400 that utilizes thesystem and methods in accordance with the present invention. FIG. 4Adepicts the tiltrotor aircraft 400 in takeoff-and-landing mode or hovermode, and FIG. 4B illustrates the tiltrotor aircraft 400 in cruise mode.Tiltrotor aircraft 400 includes proprotor assemblies 402 a and 402 bthat are carried by wings 404 a and 404 b, and are disposed at endportions 406 a and 406 b of wings 404 a and 404 b, respectively.Proprotor assemblies 402 a and 402 b include nacelles 408 a and 408 b,which include the engines and transmissions of tiltrotor aircraft 400.In this embodiment, the engines are fixed to the wing and do not rotate,rather, only the pylons 410 a and 410 b with the proprotor assemblies402 a and 402 b rotate. Proprotor assemblies 402 a and 402 b move androtate relative to wings 404 a and 404 b and the nacelles 408 a and 408b. The proprotor assemblies 402 a and 402 b do not more relative to thewings 404 a and 404 b. Instead, during the transition between ahelicopter or hover mode only the pylons 410 a and 410 b with theproprotor assemblies 402 a and 402 b rotate to redirect the thrust fromthe proprotor assemblies 402 a and 402 b. The tiltrotor aircraft 400 isstill able to fly like a conventional helicopter; and an airplane orcruise mode in which one of the rotors are tilted forward, such thattiltrotor aircraft 400 flies like a conventional propeller drivenaircraft.

FIG. 5 depicts an embodiment of the present invention, which is apassive hub flapping lock 500. This embodiment includes three similarsections, but embodiments may have two or more similar sections. In theview of FIG. 5, the flapping lock 500 is in the disengaged position toafford better visibility of components. Stop wedges 505 a, 505 b, and505 c (505 c not shown) are the components of the flapping lock 500 thatwedge between the rotor yoke 502 and the mast sleeve 507 to prevent therotor yoke 502 from flapping at low rotational speeds and whenstationary. Herein, mast sleeve 507 is pictured in the figures anddiscussed, but some aircraft may not have a mast sleeve 507 around amast. One skilled in the art of aircraft rotors and masts will recognizethat embodiments of the invention may be used with aircrafts that do nothave a mast sleeve, in which case an embodiment of the present inventionwould be arrayed around the mast, and the mast would be where mastsleeve 507 is pictured in the figures and would be discussed where themast sleeve 507 is discussed. The stop wedges, which need to providesoft yet firm resistance to hub flapping, may be made of elastomericmaterial(s) such as include one or more polymers, or one or more rubberssuch as butyl rubber, nitrile rubber, silicone rubber, or they may bemade of a foam or of soft metals such as brass or aluminum to cushionthe interface between the mast sleeve 507 and the rotor when theflapping lock 500 is engaged. Frames 510 a, 510 b, and 510 c (510 c notshown), support stop wedges 505 a, 505 b, and 505 c. The mast sleeve 507or the frames 510 a, 510 b, and 510 c may be coated with a substancesuch as TEFLON® or similar materials or coatings to reduce a friction ofthe movement of the frames 510 a, 510 b, and 510 c along the mast sleeve507 when the flapping lock 500 is in motion. Rods 515 a, 515 b, and 515c (515 c not shown) and brackets 520 a, 520 b, and 520 c (520 c notshown) connect frames 510 a, 510 b, and 510 c and stop wedges 505 a, 505b, and 505 c to the mechanisms that engage and disengage the flappinglock 500. Rod sleeves 522 a, 522 b, and 522 c may hold the rods 515 a,515 b, and 515 c in place or stabilize the rods 515 a, 515 b, and 515 c,and the rod sleeves 522 a, 522 b, and 522 c may be equipped with linearball bearings (not shown) to ease movement of the rods 515 a, 515 b, and515 c. The rod sleeves 522 a, 522 b, and 522 c may be coated with asubstance such as TEFLON® or similar materials or coatings to reduce afriction of the movement of the rod sleeves 522 a, 522 b, and 522 calong the mast sleeve 507 when the flapping lock 500 is in motion. Leverarms 525 a, 525 b, and 525 c (525 c not shown) rotate on pivots 530 a,530 b, and 530 c (530 c not shown) and are coupled to rods 515 a, 515 b,and 515 c at brackets 520 a, 520 b, and 520 c. The rods 515 a, 515 b,and 515 c may be coupled to the lever arms 525 a, 525 b, and 525 c withdirectly or with links, and the couplings may include roller bearings.Such link may also include link torsion springs (not shown). Pivottorsion springs (not shown) are at the pivots 530 a, 530 b. Weight sets535 a, 535 b, and 535 c (535 c not shown) are coupled to lever arms 525a, 525 b, and 525 c at the ends of the lever arms 525 a, 525 b, and 525c opposite ends coupled to brackets 520 a, 520 b, and 520 c. The weightsets 535 a, 535 b, and 535 c may include weights including dense metalsuch as tungsten for compactness. The weight sets 535 a, 535 b, and 535c can be adjusted to set the rotational speed at which the flapping lock500 will disengage.

When the mast sleeve 507 and rotor yoke 502 are stationary or rotatingslowly, the stop wedges 505 a, 505 b, and 505 c, frames 510 a, 510 b,and 510 c, rods 515 a, 515 b, and 515 c, and brackets 520 a, 520 b, and520 c pull the lever arms 525 a, 525 b, and 525 c down, with the aid ofthe pivot torsion springs at the pivots 530 a, 530 b, and 530 c (and, ifpresent, the link torsion springs), against the weight of the weightsets 535 a, 535 b, and 535 c, so that the stop wedges 505 a, 505 b, and505 c and frames 510 a, 510 b, and 510 c sit in the gap between the mastsleeve 507 and the rotor yoke 502 and prevent movement. When the mastsleeve 507 and rotor yoke 502 are rotating rapidly, the weight sets 535a, 535 b, and 535 c move outward, overcoming the pivot torsion springsat the pivots 530 a, 530 b, and 530 c (and, if present, the link torsionsprings), lowering the weighted ends of the lever arms 525 a, 525 b, and525 c to which they are attached and raising the ends opposite and theportions of the flapping lock that are attached to them out of the gapbetween the mast sleeve 507 and the rotor yoke 502, allowing movement.

FIG. 6 shows portions of the embodiment of the present inventionpictured in FIG. 5. In this embodiment, the flapping lock 500 includesthree similar sections. FIG. 6 illustrates a portion of one of thesesections including stop wedge 505 a, frame 510 a, rod 515 a, and bracket520 a.

FIG. 7A illustrates the flapping lock 500 in its engaged position tostop the mast sleeve 507 from flapping on the rotor yoke 502. One of thethree sections is completely visible, while two other sections arepartly visible. FIG. 7A shows stop wedge 505 a, frame 510 a, rod 515 a,bracket 520 a, lever arm 525 a, pivot 530 a, and weight set 535 a. FIG.7A also illustrates stop wedge 505 b, frame 510 b, rod 515 b, bracket520 b, and lever arm 525 b, and stop wedge 505 c, frame 510 c, rod 515c, bracket 520 c, lever arm 525 c, pivot 530 c, and weight set 535 c.

FIG. 7B shows the flapping lock 500 in its fully disengaged position.FIG. 7B illustrates all of the same components of flapping lock 500listed with regard to FIG. 7A.

FIG. 8 illustrates a flowchart of a method embodiment of the presentinvention. Method 800 for preventing rotor flapping includes block 805,providing one or more stop wedges mounted on one or more frames to beinserted into a space between a mast sleeve or a mast and a rotor yoketo prevent rotor flapping. Block 810 includes lowering the one or morestop wedges into the space when stationary or at a rotational speedbelow a specified rotational speed. Included in block 815 is raising theone or more stop wedges out of the space at the specified rotationalspeed. Block 820 includes controlling the position of the one or morestop wedges with one or more weight sets coupled to one or more leverarms that are coupled to the one or more stop wedges, wherein the one ormore weight sets move outward at the specified rotational speed, movingthe lever arms such that the one or more stop wedges are raised from thespace.

It will be understood that particular embodiments described herein areshown by way of illustration and not as limitations of the invention.The principal features of this invention can be employed in variousembodiments without departing from the scope of the invention. Thoseskilled in the art will recognize, or be able to ascertain using no morethan routine experimentation, numerous equivalents to the specificprocedures described herein. Such equivalents are considered to bewithin the scope of this invention and are covered by the claims.

All publications and patent applications mentioned in the specificationare indicative of the level of skill of those skilled in the art towhich this invention pertains. All publications and patent applicationsare herein incorporated by reference to the same extent as if eachindividual publication or patent application was specifically andindividually indicated to be incorporated by reference.

The use of the word “a” or “an” when used in conjunction with the term“comprising” in the claims and/or the specification may mean “one,” butit is also consistent with the meaning of “one or more,” “at least one,”and “one or more than one.” The use of the term “or” in the claims isused to mean “and/or” unless explicitly indicated to refer toalternatives only or the alternatives are mutually exclusive, althoughthe disclosure supports a definition that refers to only alternativesand “and/or.” Throughout this application, the term “about” is used toindicate that a value includes the inherent variation of error for thedevice, the method being employed to determine the value, or thevariation that exists among the study subjects.

As used in this specification and claim(s), the words “comprising” (andany form of comprising, such as “comprise” and “comprises”), “having”(and any form of having, such as “have” and “has”), “including” (and anyform of including, such as “includes” and “include”) or “containing”(and any form of containing, such as “contains” and “contain”) areinclusive or open-ended and do not exclude additional, unrecitedelements or method steps. In embodiments of any of the compositions andmethods provided herein, “comprising” may be replaced with “consistingessentially of” or “consisting of.” As used herein, the phrase“consisting essentially of” requires the specified integer(s) or stepsas well as those that do not materially affect the character or functionof the claimed invention. As used herein, the term “consisting” is usedto indicate the presence of the recited integer (e.g., a feature, anelement, a characteristic, a property, a method/process step, or alimitation) or group of integers (e.g., feature(s), element(s),characteristic(s), property(ies), method/process(s) steps, orlimitation(s)) only.

The term “or combinations thereof” as used herein refers to allpermutations and combinations of the listed items preceding the term.For example, “A, B, C, or combinations thereof” is intended to includeat least one of: A, B, C, AB, AC, BC, or ABC, and if order is importantin a particular context, also BA, CA, CB, CBA, BCA, ACB, BAC, or CAB.Continuing with this example, expressly included are combinations thatcontain repeats of one or more item or term, such as BB, AAA, AB, BBC,AAABCCCC, CBBAAA, CABABB, and so forth. The skilled artisan willunderstand that typically there is no limit on the number of items orterms in any combination, unless otherwise apparent from the context.

As used herein, words of approximation such as, without limitation,“about,” “substantial” or “substantially” refers to a condition thatwhen so modified is understood to not necessarily be absolute or perfectbut would be considered close enough to those of ordinary skill in theart to warrant designating the condition as being present. The extent towhich the description may vary will depend on how great a change can beinstituted and still have one of ordinary skill in the art recognize themodified feature as still having the required characteristics andcapabilities of the unmodified feature. In general, but subject to thepreceding discussion, a numerical value herein that is modified by aword of approximation such as “about” may vary from the stated value byat least ±1, 2, 3, 4, 5, 6, 7, 10, 12 or 15%.

All of the devices and/or methods disclosed and claimed herein can bemade and executed without undue experimentation in light of the presentdisclosure. While the devices and/or methods of this invention have beendescribed in terms of particular embodiments, it will be apparent tothose of skill in the art that variations may be applied to thecompositions and/or methods and in the steps or in the sequence of stepsof the method described herein without departing from the concept,spirit and scope of the invention. All such similar substitutes andmodifications apparent to those skilled in the art are deemed to bewithin the spirit, scope, and concept of the invention as defined by theappended claims.

Furthermore, no limitations are intended to the details of constructionor design herein shown, other than as described in the claims below. Itis therefore evident that the particular embodiments disclosed above maybe altered or modified and all such variations are considered within thescope and spirit of the disclosure. Accordingly, the protection soughtherein is as set forth in the claims below.

Modifications, additions, or omissions may be made to the systems andapparatuses described herein without departing from the scope of theinvention. The components of the systems and apparatuses may beintegrated or separated. Moreover, the operations of the systems andapparatuses may be performed by more, fewer, or other components. Themethods may include more, fewer, or other steps. Additionally, steps maybe performed in any suitable order.

To aid the Patent Office, and any readers of any patent issued on thisapplication in interpreting the claims appended hereto, applicants wishto note that they do not intend any of the appended claims to invoke 35U.S.C. § 112(f) as it exists on the date of filing hereof unless thewords “means for” or “step for” are explicitly used in the particularclaim.

What is claimed is:
 1. A passive hub flapping lock comprising: one ormore stop wedges; one or more frames coupled to the one or more stopwedges; one or more rods coupled to the one or more frames, and each rodcomprising a bracket; one or more lever arms, each lever arm rotatablycoupled to a pivot and coupled at a first lever arm end to one of theone or more rods at the bracket of the rod; one or more weight sets,each weight set coupled to a second lever arm end; and one or more pivottorsion springs, each pivot torsion spring positioned at a pivot andbiased to hold the flapping lock in an engaged position when stationaryor at a rotational speed below a specified rotational speed; wherein theflapping lock is in an engaged position when stationary or at arotational speed below the specified rotational speed and wherein theflapping lock is in a disengaged position when at a rotational speedabove the specified rotational speed and the one or more weight setsmove outward, rotating the one or more lever arms.
 2. The flapping lockof claim 1, wherein the one or more stop wedges comprise an elastomericmaterial, a foam, a soft metal, or a combination of two or more of thosematerials.
 3. The flapping lock of claim 1, wherein the one or more rodsare held in place or stabilized by one or more rod sleeves.
 4. Theflapping lock of claim 3, wherein at least a portion of each of the oneor more rod sleeves adjacent to a mast sleeve or a mast is coated withone or more substances to reduce a friction of a motion of the one ormore rod sleeves against the mast sleeve or the mast.
 5. The flappinglock of claim 3, wherein the rod sleeves comprise linear ball bearings.6. The flapping lock of claim 1, wherein each of the one or more leverarms is coupled to one of the one or more rods with a roller bearingdirectly or with a link.
 7. The flapping lock of claim 1, wherein eachof the one or more weight sets is adjustable to set the specifiedrotational speed.
 8. The flapping lock of claim 1, wherein at least aportion of a mast sleeve, a mast, or each frame is coated with one ormore substances to reduce a friction of a motion of the one or moreframes against the mast sleeve or the mast.
 9. A method of preventinghub flapping comprising: providing one or more stop wedges mounted onone or more frames to be inserted into a space between a mast sleeve ora mast and a rotor yoke to prevent hub flapping; lowering the one ormore stop wedges into the space when stationary or at a rotational speedbelow a specified rotational speed; raising the one or more stop wedgesout of the space at the specified rotational speed; keeping the one ormore stop wedges out of the space when above the specified rotationalspeed; and controlling a position of the one or more stop wedges withone or more weight sets coupled to one or more lever arms that arecoupled to the one or more stop wedges, wherein the one or more weightsets move outward at the specified rotational speed, moving the leverarms such that the one or more stop wedges are raised from the space.10. The method of claim 9, wherein the one or more stop wedges comprisean elastomeric material, a foam, a soft metal, or a combination of twoor more of those materials.
 11. The method of claim 9, wherein one ormore rods couple the one or more stop wedges with the one or more leverarms.
 12. The method of claim 11, wherein each of the one or more leverarms is coupled to one of the one or more rods with a roller bearingdirectly or with a link.
 13. The method of claim 11, wherein the one ormore rods are held in place or stabilized by one or more rod sleeves.14. The method of claim 13, wherein at least a portion of each of theone or more rod sleeves adjacent to the mast sleeve or the mast iscoated with one or more substances to reduce a friction of a motion ofthe one or more rod sleeves against the mast sleeve or the mast.
 15. Themethod of claim 13, wherein the one or more rod sleeves comprise linearball bearings.
 16. The method of claim 9, wherein each of the one ormore weight sets is adjustable to set the specified rotational speed.17. The method of claim 9, wherein at least a portion of the mastsleeve, the mast, or each frame is coated with one or more substances toreduce a friction of a motion of the one or more frames against the mastsleeve or the mast.
 18. A rotorcraft comprising: a fuselage; one or moreengines coupled to the fuselage; one or more rotor assemblies coupled tothe one or more engines; and each of the one or more rotor assembliescomprising a flapping lock, the flapping lock comprising: one or morestop wedges; one or more frames coupled to the one or more stop wedges;one or more rods coupled to the one or more frames, and each rodcomprising a bracket; one or more lever arms, each lever arm rotatablycoupled to a pivot and coupled at a first lever arm end to one of theone or more rods at the bracket of the rod; one or more weight sets,each weight set coupled to a second lever arm end; and one or more pivottorsion springs, each pivot torsion spring positioned at a pivot andbiased to hold the flapping lock in an engaged position when stationaryor at a rotational speed below a specified rotational speed; wherein theflapping lock is in an engaged position when stationary or at arotational speed below the specified rotational speed and in adisengaged position when at a rotational speed above the specifiedrotational speed and the one or more weight sets move outward, rotatingthe one or more lever arms.